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CFD Method for Aircraft Skid Performance Including Wear and Heat Transfer
ISSN: 0148-7191, e-ISSN: 2688-3627
Published August 19, 2008 by SAE International in United States
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A CFD method for predicting wear and heat transfer for an aircraft skid is described. It uses a finite volume method with a moving grid to account for wear. Therefore the skid material flows through the grid. The interface between the skid and runway is modeled empirically and is based on test data. A calculation for a simple skid is presented. The code is written in Mathematica which runs quickly and therefore is useful for experimenting with physical models and conducting trade studies.
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CitationCarroll, G., "CFD Method for Aircraft Skid Performance Including Wear and Heat Transfer," SAE Technical Paper 2008-01-2249, 2008, https://doi.org/10.4271/2008-01-2249.
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